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| author | debashisdeb | 2014-06-20 15:42:42 +0530 |
|---|---|---|
| committer | debashisdeb | 2014-06-20 15:42:42 +0530 |
| commit | 83c1bfceb1b681b4bb7253b47491be2d8b2014a1 (patch) | |
| tree | f54eab21dd3d725d64a495fcd47c00d37abed004 /Satellite_Communication/chapter_3.ipynb | |
| parent | a78126bbe4443e9526a64df9d8245c4af8843044 (diff) | |
| download | Python-Textbook-Companions-83c1bfceb1b681b4bb7253b47491be2d8b2014a1.tar.gz Python-Textbook-Companions-83c1bfceb1b681b4bb7253b47491be2d8b2014a1.tar.bz2 Python-Textbook-Companions-83c1bfceb1b681b4bb7253b47491be2d8b2014a1.zip | |
removing problem statements
Diffstat (limited to 'Satellite_Communication/chapter_3.ipynb')
| -rw-r--r-- | Satellite_Communication/chapter_3.ipynb | 15 |
1 files changed, 0 insertions, 15 deletions
diff --git a/Satellite_Communication/chapter_3.ipynb b/Satellite_Communication/chapter_3.ipynb index 376a12af..e87eed02 100644 --- a/Satellite_Communication/chapter_3.ipynb +++ b/Satellite_Communication/chapter_3.ipynb @@ -27,7 +27,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Inclination angle'''\n",
"import math\n",
"#Variable Declaration\n",
"Az=85 # Azimuth angle of injection point\n",
@@ -68,7 +67,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Velocity thrust'''\n",
"import math\n",
"#Variable Declaration\n",
"delta_i=7 #orbital plane inclination\n",
@@ -107,7 +105,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''velocity thrust'''\n",
"import math\n",
"\n",
"#Variable Declaration\n",
@@ -152,7 +149,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Thrust velocity'''\n",
"import math\n",
"#Variable Declaration\n",
"A=15000*10**3 #Original apogee distance\n",
@@ -195,7 +191,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Thrust velocity'''\n",
"import math\n",
"#Variable Declaration\n",
"A=15000.0*10**3 # Original apogee distance\n",
@@ -237,7 +232,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Thrust velocity '''\n",
"#Variable Declaration\n",
"A=15000.0*10**3 # Original apogee distance\n",
"A1=16000.0*10**3 # Raised opogee distance\n",
@@ -279,7 +273,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Thrust velocity'''\n",
"import math\n",
"#Variable Declaration\n",
"R=6378.0*10**3 # Radius of earth\n",
@@ -325,7 +318,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Maximum line-of-sight distance'''\n",
"import math\n",
"#Variable Declaration\n",
"H=36000.0 # Height of geostationary satellite from the surface of earth\n",
@@ -368,7 +360,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "''' line-of-sight distance'''\n",
"import math\n",
"#Variable Declaration\n",
"H=36000.0 # Height of geostationary satellite from the surface of earth\n",
@@ -410,7 +401,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Inter-satellite distance'''\n",
"import math\n",
"\n",
"#Variable Declaration\n",
@@ -456,7 +446,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Azimuth and elevation angle'''\n",
"import math\n",
"\n",
"theta_l=30.0 # earth station's location 30\u00b0W longitude\n",
@@ -501,7 +490,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Time Delay'''\n",
"import math\n",
"#Variable Declaration\n",
"theta_l=60.0 #earth station's location 60\u00b0W longitude\n",
@@ -610,7 +598,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Inter-satellite distance'''\n",
"import math\n",
"#Variable Declaration\n",
"da=38000.0 # slant range of satellite A\n",
@@ -657,7 +644,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''covered surface area'''\n",
"import math\n",
"#Variable Declaration\n",
"r=42164.0 # orbital radius of the satellite in km\n",
@@ -726,7 +712,6 @@ "cell_type": "code",
"collapsed": false,
"input": [
- "'''Area swept by ground track of sattelite'''\n",
"#variable declaration\n",
"theta=30 #satellite inclination to the equitorial plan\n",
"#the extreme latitudes covered in northern and southern hemisphere are the same as orbit inclination\n",
|